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HECK NO the globe pattern offers the most pressure drop because of friction losses
Simple answer: Yes.
Pressure drop is a term used to describe the decrease in pressure from one point in a pipe or tube to another point downstream.This occurs when flow resistance resulting in frictional forces acts on the fluid while it is flowing through a tube. The major identifiers of the resistance include fluid viscosity and fluid velocity in the pipe. Pressure drop elevates the same way as shear forces inside the piping network. alliedallcityinc.com
gas turbines and gas engines are different in mechanic designes uses diffrent liquid for engine we use flemmable gas we use for turbine liquide flemmable but they need air both gas turbines and gas engines are different in mechanic designes uses diffrent liquid for engine we use flemmable gas we use for turbine liquide flemmable but they need air both answer by nailiyoucef05@yahoo.fr I dont think so. Gas engine works as the same principle of a petrol engine. And in gas turbine gas is burned and high velocity gas is passed through the turbine. A gas engine is an internal combustion engine and have no turbines. alamm2@asme.org
(to check the flow rate of water ... calculate the pressure drop
The difference between impulse and reaction turbine goes here...... 1) In case of an impulse turbine the pressure remains same in the rotor or runners, but in case of reaction turbine the pressure decreases in runners as well as stators also. 2) In case of impulse turbine the pressure drop happens only in the nozzle part by means of its kinetic energy. In case of Reaction one the stators those are fixed to the diaphragm act as a nozzle.
It is generally based on the Type of rotor ( Impulse/ curtis) and the enthalpy drop per stage.
A condensing turbine uses all the energy from the steam going from high pressure turbine to secondary turbine to condensing turbine then sends the condensate back for reheating. where a non condensing turbine just uses the high pressure aspect of the steam then returns the low pressure stream back to be reheated. Condensng turbines utilises the entire available drop from high pressure to the vacuum in the condenser; a back pressure turbine only utilises only the top part, whereas an exhaust steam turbine utilises only th bottom part of the pressure drop. Hope that helps.
the arterioles
Yes, increase in pressure causes the freezing point to drop.
Isolating valves may have passing.
In the low pressure side of a steam turbine, the vacuum is maintained by the condensation of steam in the condenser. At high loads, the condenser may not satisify the demand, allowing steam to remain gaseous for a longer period of time. This can cause pressure to rise.
From what I have read, it uses the heat of vaporization to create a vacuum due to condensation. So as steam condenses its volume is reduced. This creates a vacuum which increases the pressure drop accross the turbine. The larger the pressure drop accross the turbine, the better. I'm not an expert tho... http://books.google.com/books?id=7PeSdVhFhxgC&pg=PA41&lpg=PA41&dq=why+condenser&source=web&ots=HTeczt_DhL&sig=QS5YkcFzMQkTomz5y5FMb_Swsio&hl=en&sa=X&oi=book_result&resnum=1&ct=result
Firstly, vacuum is being created in turbine exhaust and condenser rather than being required. It is created to reduce the back-pressures and to improve the turbine efficiency. Also, with vacuum the designers can design large size last stage blades of LP turbine for maximizing the turbine output.
It is the ratio of cumulative heat drop to isentropic heat drop in a multistage steam turbine.
the efficiency of rocket propellant is called specific impulse the more the specific impulse the more the performance .
Thats for me to know and you to find out.